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Bending Stresses in Beams

Theory of simple bending and its assumptions, the flexure formula M/I = σ/y = E/R, neutral axis, section modulus of standard sections, economical sections, strongest and stiffest rectangular beam from a log, unsymmetrical sections, flitched (composite) beams and beams of uniform strength — with solved numericals.

📑 Contents (10 sections)

Last reviewed 16 Sept 2026 · 8 min read

Pure bending

A beam segment carrying a bending moment with no shear force is in pure (simple) bending — for example, the middle portion of a simply supported beam with two equal loads placed symmetrically. The theory below is exact for pure bending and is used, with negligible error, where shear is also present.

When a beam sags, its top fibres shorten and its bottom fibres lengthen. Somewhere between lies a layer that neither shortens nor lengthens: the neutral layer. Its intersection with a cross-section is the neutral axis (NA).

Assumptions of the theory of simple bending

  1. The material is homogeneous, isotropic and obeys Hooke's law; stresses are within the elastic limit.
  2. is the same in tension and compression.
  3. Plane sections remain plane after bending (Bernoulli–Euler hypothesis).
  4. The beam is initially straight and every layer is free to expand or contract independently.
  5. The radius of curvature is large compared with the depth.
  6. The loads act in a plane of symmetry of the section (so the beam bends without twisting).

The flexure formula

Consider a layer at distance from the neutral layer, which bends to radius . Its original length equals the neutral-layer length ; after bending it is . So its strain is

Stress is proportional to the distance from the neutral axis.

  • Force equilibrium (no net axial force): → → the neutral axis passes through the centroid of the section.
  • Moment equilibrium: .
FormulaBending equation

= bending moment, = second moment of area about the neutral axis, = bending stress at distance from the NA, = Young's modulus, = radius of curvature of the neutral layer. is the flexural rigidity.

FigureBending stress distribution across a rectangular section (sagging)

N.A.d/2compression σctension σtzero stress

Linear distribution: zero at the neutral axis, maximum at the extreme fibres.

Section modulus and moment of resistance

The maximum stress occurs at the extreme fibre, :

is the section modulus. For a permissible stress , the moment of resistance is . The beam is safe if . A larger means a stronger section in bending.

Section about centroidal axis
Rectangle (bending about the side)
Square of side
Square with diagonal vertical
Solid circle, diameter
Hollow circle ,
Hollow rectangle outer, inner
Triangle, base , height (base horizontal) (to apex), (to base)
Exam TipDoubling depth versus doubling width

For a rectangle . Doubling the width doubles the strength; doubling the depth makes it four times stronger (and eight times stiffer, since ). This is why beams are placed with the longer side vertical.

Economical sections

Most of the bending resistance comes from material far from the neutral axis, where stress is high. Material near the NA is lightly stressed. I-sections and box sections put most material in the flanges, giving a large for a small area — the most economical shapes for steel beams.

Comparing shapes of equal area

  • Square vs circle (same area): — the square is stronger.
  • Square with a side horizontal vs diagonal vertical: ratio — the square resting on a side is stronger.
  • I-section vs rectangle of the same area and depth: the I-section is several times stronger.

Strongest and stiffest rectangular beam cut from a round log of diameter

With :

  • Strongest (maximum ): , , so .
  • Stiffest (maximum ): , , so .

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